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Error while validating rdl content

Photometric informational method for unmanned aerial vehicles localization. Static stability of a helicopter main rotor flexible blade at the parking affected by wind. Solar thermal rocket engine with beryllium-oxide phase-transition latent heat energy storage and hydrogen afterburning. Developing calculation method for forced vibrations of turbomachines of a blisk type blades. Spacecraft solar batteries dynamic analysis. Holes formation mechanism while laser perforation of metallized thermal vacuum blanket films. Risk of problem solution skills loss by civil aviation pilots in uncertainty conditions. Experimental study of radiofrequency cathode-neutralizer.

Error while validating rdl content


Analysis of application specifics of a reaction wheel with intrinsic disturbing moments compensation. Evaluation of destructive rotation frequency of turbo-machine disks applying deformation criterion with LS-DYNA software. Parameters selection of space debris removal system with elastic elements by cable towing. Risk of problem solution skills loss by civil aviation pilots in uncertainty conditions. A method of light alloys reinforcing by aero-thermoacoustic treatment for aerospace industry. Work process of the earth environments vortex formation. Computer aided design and computing of a plate-type heat exchanger for small-size gas turbine engine. Developing calculation method for forced vibrations of turbomachines of a blisk type blades. Evaluation of layered aluminum-fiberglass plastic effective mechanical characteristics in conditions of uniaxial tensile. A spacecraft solar batteries panels strength calculation. Automated system for space vehicle status monitoring. Development of prospective multipurpose convertiplane. Determining resultant current harmonic composition of an electric motor symmetric four-phase winding. Docking with space debris employing the unfolding flexible beam-strap. Wings aerodynamic optimization technique for small-sized unmanned aerial vehicles. Holes formation mechanism while laser perforation of metallized thermal vacuum blanket films. Hybrid energy storage device in power supply system for prospective spacecraft. Electromecanical complex with high-frequency induction drive for gas-turbine engine. Effect of centrifugal mass forces on heat transfer when airflow of concave surface with transverse projections. Electric power supply system with distributed differential high voltage dc-link and modular-scalable architecture for all-electric aircraft. Static stability of a helicopter main rotor flexible blade at the parking affected by wind. Multiphase pulse-width modulators for devices with a multichannel principle of electric power conversion. Finite element method application for determining water landing parameters of airplanes and helicopters of various types. Structure selection of synchronous motor with permanent magnets and asynchronous start-up. High-tech production managing with account for requirements of economic security on the example of aircraft building. Development of effective forms of production process stuffing in aircraft building industry.

Error while validating rdl content


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